Wing and propeller aerodynamic interaction through nonlinear lifting line theory and blade element momentum theory
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F18%3A00330373" target="_blank" >RIV/68407700:21220/18:00330373 - isvavai.cz</a>
Result on the web
<a href="https://www.matec-conferences.org/articles/matecconf/abs/2018/92/matecconf_easn_ceas2018_00027/matecconf_easn_ceas2018_00027.html" target="_blank" >https://www.matec-conferences.org/articles/matecconf/abs/2018/92/matecconf_easn_ceas2018_00027/matecconf_easn_ceas2018_00027.html</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1051/matecconf/201823300027" target="_blank" >10.1051/matecconf/201823300027</a>
Alternative languages
Result language
angličtina
Original language name
Wing and propeller aerodynamic interaction through nonlinear lifting line theory and blade element momentum theory
Original language description
In this paper a computational methodology of aerodynamic interaction between propeller and wing is described. Presented work is focused on development of quick and accurate tool. Lifting line theory (LLT) with nonlinear airfoil characteristic is used to solve a finite span wing aerodynamic to predict downwash and lift distribution respectively. Blade element momentum theory (BEM) is used as a computational tool for estimating total thrust, torque, axial and tangential velocity distributions. Model of slipstream development is considered. Influence of propeller model to wing is simulated as contribution of higher dynamic pressure and change of angle of attack behind the propeller
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
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OECD FORD branch
20304 - Aerospace engineering
Result continuities
Project
<a href="/en/project/EF16_019%2F0000826" target="_blank" >EF16_019/0000826: Center of Advanced Aerospace Technology</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2018
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
8th EASN-CEAS International Workshop on Manufacturing for Growth & Innovation
ISBN
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ISSN
2261-236X
e-ISSN
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Number of pages
8
Pages from-to
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Publisher name
MATEC
Place of publication
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Event location
Glasgow
Event date
Sep 4, 2018
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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